Engineering, 22.11.2019 02:31 heleneallie7ou1fnk

The turbine section in a jet engine receives gas (assume air) at 1200 k, 800 kpa with an ambient atmosphere at 80 kpa. the turbine is followed by a nozzle open to the atmosphere, and all the turbine work drives a compressor. find the turbine exit pressure so that the nozzle has an exit velocity of 800 m/s.

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The turbine section in a jet engine receives gas (assume air) at 1200 k, 800 kpa with an ambient atm...